Description
History
The aircraft was originally delivered new from Piper, Florida to Denmark in June 2000 and subsequently operated by an Aeroclub in Italy from 2001.
In April 2005, the aircraft experienced a runway excursion during takeoff in Zell am See. The aircraft was professionally repaired in 2006 by a certified maintenance facility in Germany.
The current owner acquired the aircraft in June 2008, following a comprehensive overhaul including engines, propellers, landing gear and avionics. In September 2008, a minor propeller contact during landing occurred, which was properly inspected and addressed.
Since then, the aircraft has been continuously operated and maintained with no further incidents reported.
Aircraft Subject to Prior Sale or Removal from Market without Notice. Specification Subject to Verification by Purchaser.Spécifications
Année2000
fabricant PIPER
ModèleSENECA V
Numéro de série3449168
Registration #D-GREA
EtatOccasion
FlightRulesIFR
Total Time3,100
AirframeMake / Model: Piper PA-34-220T Seneca V
Year: 2000
Serial Number: 3449168
Total Time: 3100 h TT
Engine 1 Make/ModelCONTINENTAL TSIO360RB
Engine 1 Horsepower164.05 kW
Engine 1 Time1,462 SMOH
Engine 1 TBO2000
Engine(s)Continental (L)TSIO-360-RB, rated at 220 hp
TBO 2.000 hr or 12 years recommended
L/H 1.462 SMOH compl. in 02/2006
leak test: 70/72/70/70/70/70 of 80 psi
R/H 1.462 SMOH compl. in 02/2006
leak test: 78/68/74/70/76/68 of 80 psi
Engine 2 Make/ModelCONTINENTAL TSIO360RB
Engine 2 Horsepower164.05 kW
Engine 2 Time1,462 SMOH
Engine 2 NotesContinental (L)TSIO-360-RB, rated at 220 hp
TBO 2.000 hr or 12 years recommended
L/H 1.462 SMOH compl. in 02/2006
leak test: 70/72/70/70/70/70 of 80 psi
R/H 1.462 SMOH compl. in 02/2006
leak test: 78/68/74/70/76/68 of 80 psi
Prop 1 ManufacturerMCCAULEY
Prop 1 Model3AF32C523
Temps d'hélice 145 SOH
Prop 2 ManufacturerMCCAULEY
Prop 2 Model3AF32C523
Temps d'hélice 245 SOH
Nombre de lames3
Prop SpecsMcCauley 3AF32C523/(L)82NJA-6, 3-blade
TBO 2.000 hr or 6 years recommended
L/H + R/H: 45 SPOH compl. in 02/2025
Avionics/RadiosAudio/Marker Garmin GMA-340
COM/NAV/GPS Garmin dual GNS-430
Transponder Garmin GTX-330
ADF S-Tec ADF-650A
DME S-Tec TCR-451
Autopilot / Flight Director S-Tec System 55
ALT preselct S-Tec ST-360
WX Radar King KDR-2000
ELT Artex ME-406
Additional EquipmentBoots
Propeller De-Ice
Windshield heat
GND clearance switch
Co-pilot instruments
Exterior NotesAllover White with Blue stripes in good condition (7 of 10)
Interior NotesGrey Leather Interior in good condition (7 of 10)
Inspection StatusAnnual: July
Maintenance: The aircraft has been continuously maintained in accordance with Part-ML under an approved Aircraft Maintenance Programme (AMP), ensuring a well-documented and fully traceable maintenance history.
A comprehensive 50-hour / 100-hour inspection together with the Airworthiness Review was completed in July 2026. The aircraft was found airworthy and is supported by a valid ARC until 20 July 2027. All applicable ADs and LTAs have been complied with in accordance with the approved maintenance programme.
Recent maintenance included extensive system inspections, engine runs, landing gear functional checks including emergency extension, avionics testing, inspection of engine and airframe flexible hoses, vacuum pump wear checks, replacement of both vacuum regulator filters and the completion of all scheduled maintenance items. Both engines successfully completed the required ground runs and functional checks.
Overall, the aircraft presents itself in a technically sound, well-maintained and operationally ready condition with its latest scheduled maintenance and airworthiness review completed.
AirworthyOui
Année2000|
fabricant PIPER|
ModèleSENECA V|
Numéro de série3449168|
Registration #D-GREA|
EtatOccasion|
FlightRulesIFR|
Total Time3,100|
AirframeMake / Model: Piper PA-34-220T Seneca V
Year: 2000
Serial Number: 3449168
Total Time: 3100 h TT|
Engine 1 Make/ModelCONTINENTAL TSIO360RB |
Engine 1 Horsepower164.05 kW|
Engine 1 Time1,462 SMOH |
Engine 1 TBO2000|
Engine(s)Continental (L)TSIO-360-RB, rated at 220 hp
TBO 2.000 hr or 12 years recommended
L/H 1.462 SMOH compl. in 02/2006
leak test: 70/72/70/70/70/70 of 80 psi
R/H 1.462 SMOH compl. in 02/2006
leak test: 78/68/74/70/76/68 of 80 psi|
Engine 2 Make/ModelCONTINENTAL TSIO360RB |
Engine 2 Horsepower164.05 kW|
Engine 2 Time1,462 SMOH |
Engine 2 NotesContinental (L)TSIO-360-RB, rated at 220 hp
TBO 2.000 hr or 12 years recommended
L/H 1.462 SMOH compl. in 02/2006
leak test: 70/72/70/70/70/70 of 80 psi
R/H 1.462 SMOH compl. in 02/2006
leak test: 78/68/74/70/76/68 of 80 psi|
Prop 1 ManufacturerMCCAULEY|
Prop 1 Model3AF32C523|
Temps d'hélice 145 SOH |
Prop 2 ManufacturerMCCAULEY|
Prop 2 Model3AF32C523|
Temps d'hélice 245 SOH |
Nombre de lames3|
Prop SpecsMcCauley 3AF32C523/(L)82NJA-6, 3-blade
TBO 2.000 hr or 6 years recommended
L/H + R/H: 45 SPOH compl. in 02/2025|
Avionics/RadiosAudio/Marker Garmin GMA-340
COM/NAV/GPS Garmin dual GNS-430
Transponder Garmin GTX-330
ADF S-Tec ADF-650A
DME S-Tec TCR-451
Autopilot / Flight Director S-Tec System 55
ALT preselct S-Tec ST-360
WX Radar King KDR-2000
ELT Artex ME-406|
Additional EquipmentBoots
Propeller De-Ice
Windshield heat
GND clearance switch
Co-pilot instruments|
Exterior NotesAllover White with Blue stripes in good condition (7 of 10)|
Interior NotesGrey Leather Interior in good condition (7 of 10)|
Inspection StatusAnnual: July
Maintenance: The aircraft has been continuously maintained in accordance with Part-ML under an approved Aircraft Maintenance Programme (AMP), ensuring a well-documented and fully traceable maintenance history.
A comprehensive 50-hour / 100-hour inspection together with the Airworthiness Review was completed in July 2026. The aircraft was found airworthy and is supported by a valid ARC until 20 July 2027. All applicable ADs and LTAs have been complied with in accordance with the approved maintenance programme.
Recent maintenance included extensive system inspections, engine runs, landing gear functional checks including emergency extension, avionics testing, inspection of engine and airframe flexible hoses, vacuum pump wear checks, replacement of both vacuum regulator filters and the completion of all scheduled maintenance items. Both engines successfully completed the required ground runs and functional checks.
Overall, the aircraft presents itself in a technically sound, well-maintained and operationally ready condition with its latest scheduled maintenance and airworthiness review completed.|
AirworthyOui|
